ES8102198A1 - Process for the manufacture of hollow bodies of an aluminium alloy, and products thus obtained. - Google Patents
Process for the manufacture of hollow bodies of an aluminium alloy, and products thus obtained.Info
- Publication number
- ES8102198A1 ES8102198A1 ES491989A ES491989A ES8102198A1 ES 8102198 A1 ES8102198 A1 ES 8102198A1 ES 491989 A ES491989 A ES 491989A ES 491989 A ES491989 A ES 491989A ES 8102198 A1 ES8102198 A1 ES 8102198A1
- Authority
- ES
- Spain
- Prior art keywords
- products
- hollow bodies
- manufacture
- aluminium alloy
- bursting strength
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/10—Alloys based on aluminium with zinc as the next major constituent
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Continuous Casting (AREA)
- Pressure Vessels And Lids Thereof (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Extrusion Of Metal (AREA)
Abstract
The invention relates to a process for obtaining hollow bodies made of aluminum alloy having a high bursting strength, and to the products thus obtained. The alloy contains (by weight): from 7.6 to 9.5% of Zn from 1 to 1.8% of Cu from 2.4 to 3.5% of Mg from 0.07 to 0.17% of Cr from 0.15 to 0.25% of Mn from 0.08 to 0.14% of Zr less than 0.2% of Fe, 0.15% of Si 0.10% of Ti and optionally less than 0.01% of V. It has a tensile stress (lengthwise direction) and a bursting strength (transverse direction) greater than or equal to 660 MPa. Its structure is characterized by the absence of large intermetallic compounds (>35 mu m) after a specific solidification test. It can be used in all the safety applications involving a container under pressure (bottles of compressed gas, etc.).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7915054A FR2457908A1 (en) | 1979-06-01 | 1979-06-01 | PROCESS FOR PRODUCING HOLLOW BODIES OF ALUMINUM ALLOY AND PRODUCTS THUS OBTAINED |
Publications (2)
Publication Number | Publication Date |
---|---|
ES8102198A1 true ES8102198A1 (en) | 1980-12-16 |
ES491989A0 ES491989A0 (en) | 1980-12-16 |
Family
ID=9226502
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES491989A Granted ES491989A0 (en) | 1979-06-01 | 1980-05-30 | MANUFACTURING PROCEDURE FOR ALUMINUM ALLOY HOLLOW BODIES RESISTANT TO INTERNAL PRESSURE |
Country Status (11)
Country | Link |
---|---|
US (1) | US4345951A (en) |
EP (1) | EP0020282B1 (en) |
BE (1) | BE883565A (en) |
CA (1) | CA1118190A (en) |
CH (1) | CH644402A5 (en) |
DE (1) | DE3061495D1 (en) |
ES (1) | ES491989A0 (en) |
FR (1) | FR2457908A1 (en) |
IT (1) | IT1130700B (en) |
NO (1) | NO153184C (en) |
ZA (1) | ZA803235B (en) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4863528A (en) * | 1973-10-26 | 1989-09-05 | Aluminum Company Of America | Aluminum alloy product having improved combinations of strength and corrosion resistance properties and method for producing the same |
FR2517702B1 (en) * | 1981-12-03 | 1985-11-15 | Gerzat Metallurg | |
US5221377A (en) * | 1987-09-21 | 1993-06-22 | Aluminum Company Of America | Aluminum alloy product having improved combinations of properties |
FR2640644B1 (en) * | 1988-12-19 | 1991-02-01 | Pechiney Recherche | PROCESS FOR OBTAINING "SPRAY-DEPOSIT" ALLOYS FROM AL OF THE 7000 SERIES AND COMPOSITE MATERIALS WITH DISCONTINUOUS REINFORCEMENTS HAVING THESE ALLOYS WITH HIGH MECHANICAL RESISTANCE AND GOOD DUCTILITY |
JP3737105B2 (en) * | 1993-04-15 | 2006-01-18 | ラクスファー・グループ・リミテッド | Method for manufacturing hollow body |
FR2716896B1 (en) * | 1994-03-02 | 1996-04-26 | Pechiney Recherche | Alloy 7000 with high mechanical resistance and process for obtaining it. |
US5496426A (en) * | 1994-07-20 | 1996-03-05 | Aluminum Company Of America | Aluminum alloy product having good combinations of mechanical and corrosion resistance properties and formability and process for producing such product |
CN1489637A (en) | 2000-12-21 | 2004-04-14 | �Ƹ��� | Aluminum alloy products and artificial aging method |
FR2838136B1 (en) * | 2002-04-05 | 2005-01-28 | Pechiney Rhenalu | ALLOY PRODUCTS A1-Zn-Mg-Cu HAS COMPROMISED STATISTICAL CHARACTERISTICS / DAMAGE TOLERANCE IMPROVED |
FR2838135B1 (en) * | 2002-04-05 | 2005-01-28 | Pechiney Rhenalu | CORROSIVE ALLOY PRODUCTS A1-Zn-Mg-Cu WITH VERY HIGH MECHANICAL CHARACTERISTICS, AND AIRCRAFT STRUCTURE ELEMENTS |
ES2292075T5 (en) | 2005-01-19 | 2010-12-17 | Otto Fuchs Kg | ALUMINUM ALLOY NOT SENSITIVE TO BRUSH COOLING, AS WELL AS A PROCEDURE FOR MANUFACTURING A SEMI-FINISHED PRODUCT FROM THIS ALLOY. |
US8083871B2 (en) | 2005-10-28 | 2011-12-27 | Automotive Casting Technology, Inc. | High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting |
US8673209B2 (en) * | 2007-05-14 | 2014-03-18 | Alcoa Inc. | Aluminum alloy products having improved property combinations and method for artificially aging same |
US8840737B2 (en) * | 2007-05-14 | 2014-09-23 | Alcoa Inc. | Aluminum alloy products having improved property combinations and method for artificially aging same |
US8206517B1 (en) | 2009-01-20 | 2012-06-26 | Alcoa Inc. | Aluminum alloys having improved ballistics and armor protection performance |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB552972A (en) * | 1942-06-12 | 1943-05-03 | Nat Smelting Co | Improvements in or relating to aluminium base alloys |
FR1322510A (en) * | 1962-05-02 | 1963-03-29 | Aluminum Co Of America | Improvement of articles in aluminum-based alloy obtained by heat treatment |
DE2052000C3 (en) * | 1970-10-23 | 1974-09-12 | Fa. Otto Fuchs, 5882 Meinerzhagen | Use of a high-strength aluminum alloy |
US4305763A (en) * | 1978-09-29 | 1981-12-15 | The Boeing Company | Method of producing an aluminum alloy product |
-
1979
- 1979-06-01 FR FR7915054A patent/FR2457908A1/en active Granted
-
1980
- 1980-05-28 DE DE8080420064T patent/DE3061495D1/en not_active Expired
- 1980-05-28 EP EP80420064A patent/EP0020282B1/en not_active Expired
- 1980-05-29 IT IT22416/80A patent/IT1130700B/en active
- 1980-05-30 BE BE0/200831A patent/BE883565A/en not_active IP Right Cessation
- 1980-05-30 ES ES491989A patent/ES491989A0/en active Granted
- 1980-05-30 NO NO801611A patent/NO153184C/en unknown
- 1980-05-30 CA CA000353060A patent/CA1118190A/en not_active Expired
- 1980-05-30 US US06/155,116 patent/US4345951A/en not_active Expired - Lifetime
- 1980-05-30 ZA ZA00803235A patent/ZA803235B/en unknown
- 1980-05-30 CH CH421480A patent/CH644402A5/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
NO801611L (en) | 1980-12-02 |
ZA803235B (en) | 1981-05-27 |
NO153184C (en) | 1986-01-29 |
EP0020282A1 (en) | 1980-12-10 |
BE883565A (en) | 1980-12-01 |
EP0020282B1 (en) | 1982-12-29 |
IT8022416A0 (en) | 1980-05-29 |
FR2457908B1 (en) | 1984-03-02 |
US4345951A (en) | 1982-08-24 |
ES491989A0 (en) | 1980-12-16 |
NO153184B (en) | 1985-10-21 |
CA1118190A (en) | 1982-02-16 |
FR2457908A1 (en) | 1980-12-26 |
DE3061495D1 (en) | 1983-02-03 |
IT1130700B (en) | 1986-06-18 |
CH644402A5 (en) | 1984-07-31 |
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